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Advanced Manifolds for Improved Solid Oxide Electrolyzer PerformanceAn investigation was conducted to see if additive manufacturing could be used to fabricate more efficient manifold designs for improved flow, reduced stresses, and decreased number of joints to be sealed for a solid oxide electrolyzer used to convert carbon dioxide to oxygen. Computational flow and mechanical modeling were conducted on a NASA Glenn Research Center patented cell and stack design with the potential to achieve a 3-4 times mass reduction. Various manifold designs were modeled, and two were downselected to be fabricated and tested. Some benefit was seen in a baffled manifold design, which directed incoming flow more effectively into the flow channels, compared to the original design, where the flow spent more time within the manifold itself. Flow measurements indicated some non-uniformity of flow across the channels at higher flow rates, which were not predicted by the model. Some possible explanations for the differences are discussed.
Document ID
20180008610
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Linne, Diane L.
(NASA Glenn Research Center Cleveland, OH, United States)
Kuczmarski, Maria A.
(NASA Glenn Research Center Cleveland, OH, United States)
Johnston, James C.
(NASA Glenn Research Center Cleveland, OH, United States)
Farmer, Serence C.
(NASA Glenn Research Center Cleveland, OH, United States)
Green, Robert D.
(NASA Glenn Research Center Cleveland, OH, United States)
Mital, Subodh K.
(Toledo Univ. Toledo, OH, United States)
Setlock, John A.
(Toledo Univ. Toledo, OH, United States)
Date Acquired
December 18, 2018
Publication Date
September 17, 2018
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN60277
Meeting Information
Meeting: Space 2018
Location: Orlando, Florida
Country: United States
Start Date: September 17, 2018
End Date: September 19, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNC13BA10B
WBS: WBS 663323.05.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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